Corpus ID: 107076331

Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control

@inproceedings{Yechout2003IntroductionTA,
  title={Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control},
  author={Thomas R. Yechout and Steven L. Morris},
  year={2003}
}
  • Thomas R. Yechout, Steven L. Morris
  • Published 2003
  • Engineering
  • A Review of Basic Aerodynamics A Review of Basic Propulsion Aircraft Performance Aircraft Equations of Motion Aircraft Static Stability Linearizing the Equations of Motion Aircraft Dynamic Stability Classical Feedback Control Aircraft Stability/Control Augmentation Special Topics Appendices. 

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    References

    Publications referenced by this paper.
    SHOWING 1-10 OF 10 REFERENCES

    Measurements of Pressures

    • J. S. Bowman, Jr., R. S. Hultberg, C. A. Martin
    • Jet,’’ Proceedings of the 2001 AIAA Guidance,
    • 2001

    X-38 Mid-Rudder Feasibility

    • AIAA, Reston, +3 authors T. R. Yechout
    • 1998

    Low Speed Rotary Aerodynamic of F-18 Configuration for 0 to 90 Angle

    • McGraw-Hill, New York, R. 1985. Hultberg
    • 1985

    Attack—Test Results and Analysis,’

    • D J., W. H. Heiser, D. H. Daley
    • NASA CR-3608,
    • 1984

    A-10A Prototype Task II Performance and Flying Qualities Evaluation,’

    • J. A. 2Papa, A. F. Douglas, J. H. Markwardt, L. D. Fortner
    • Air Force Flight Test Center TR 73-7,
    • 1973

    Other 1940s era autopilots used on military aircraft

    • Honeywell, Inc
    • 1940